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DISRUPTING AN INDUSTRY THE INDUSTRIALIZATION OF PROPULSION SYSTEMS A CASE STUDY Case study on the industrialization of propulsion systems for constellations Scaling production capabilities Product assurance at high production rates Lean manufacturing in the space industry Implementation in the ENPULSION manufacturing process Conclusion 02 04 08 10 14 20 CONTENTS
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Page 1: THE INDUSTRIALIZATION OF PROPULSION SYSTEMS … · An example for such implementation is an automatized incoming inspection tool that enables paral- ... To accomplish high throughput

DISRUPTINGAN INDUSTRYT H E I N D U S T R I A L I Z A T I O N O F P R O P U L S I O N S Y S T E M S

A C A S E S T U D Y

Case study on the industrialization of propulsion systems for constellations

Scaling production capabilities

Product assurance at high production rates

Lean manufacturing in the space industry

Implementation in the ENPULSION manufacturing process

Conclusion

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CONTENTS

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04 05

Having evolved into a viable market, the majority of business cases based on Micro- and Smallsats are

based on constellations. Rate of production as well as streamlined integration become key drivers for

success and result in flow down requirements for all subsystems.

Traditionally, this has proven to be particularly demanding for a propulsion subsystem, due to com-

plexity of most propulsion subsystems, which in turn drives the complexity of integration, as well

as strong dependability of propulsion design on mission requirements. Especially the latter has led

to one-akind implementation of propulsion systems, and therefore complex implementations, long

leadand cycle times, and therefore increased cost.

CASE STUDY ON THE INDUSTRIALIZATION OFPROPULSION SYSTEMS FOR CONSTELLATIONSA pr ac t ic al e xample on how to achie ve high pro duc t ion r ate s and low

pro duc t cos t s without compromising on her it age qualit y re quirement s .

B A C K G R O U N D

To counter such issues and comply with constellation production rate and im-

plementation requirements, ENPULSION has introduced a modular, universal

building-block based propulsion technology which is designed for high rate

production.

This IFM thruster technology has been successfully industrialized and is cur-

rently delivered to customers at unmatched rates between 2 to 5 flight pro-

pulsion systems per week.

M O D U L A R S O L U T I O N S

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06 07

Based on a product designed for high rate production, ENPULSION has implemented an adaptable

production line, that enables different scalability steps. Based on a heritage laboratory process of

thruster production, a first scalability step has already been performed by the introduction of batch

processes, increasing production capability from 1 ion emitter per week to 5 per week.

Introduction of statistical evaluation of ongoing production processes, optimized selection at early

production steps and semi-automatization allows scalability to 2 emitters per day. Further increasing

batch sizes by scaling production equipment at the existing production facility allows for production

rates of 6 emitters per day. The possibility for further scaling of such a model fabrication line by direct

multiplication of facilities and corresponding scaling of support processes makes this concept ad-

aptable to megaconstellation production rates.

SCALING PRODUCTION CAPABILITIES

A D A P T I O N

Scalability of ENPULSION production line

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10 11

There has been a general perception within the New Space Community that increasing production

rates to constellation requirements together with cost pressure necessarily leads to a tradeoff against

heritage product assurance standards (e.g. ECSS), given the significant time and effort required to

include implementation of such standards.

In contrast, ENPULSION has been successful in implementation of heritage quality processes within

the current high rate production rate, based on an agile implementation of traditional product assur-

ance (PA) processes.

With focus on optimization of PA process execution, the additional implementation effort is compen-

sated by the large number of systems produced. The definition and design of the agile implementa-

tion of heritage PA processes has been guided and complimented by a direct dialogue with space

heritage providers to find optimized implementation complying with both stringent requirements and

series production mindset.

PRODUCT ASSURANCE ATHIGH PRODUCTION RATES

A G I L E P R O C E S S E S

Optimization of mandatory inspection point (MIP) loops allow implementation with minimum delay by

designing the production and testing flow adaptable in a way so that flagged hardware can be taken

out of the manufacturing flow and reintroduced after customer decision. This is complemented with

a choice of proper tools, both digital and measurement systems, which are both optimized for high

throughput, short cycle times and digital implementation.

An example for such implementation is an automatized incoming inspection tool that enables paral-

lelized inspection of up to 100 parts, fast measurement cycle times compatible with the production

flow and automatized non-conformance reporting implementation for optimized feedback loop to

suppliers, therefore enabling 100% inspection at current and planned production rates.

F I N D I N G T H E P E R F E C T T O O L S

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12 13

LEAN MANUFACTURING IN THE SPACE INDUSTRY

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6 steps of lean manufacturing at ENPULSION high rate space propulsion production

To accomplish high throughput production without trading cost versus quality, a lean manufacturing

approach has been introduced into the ENPULSION manufacturing philosophy. In this approach, the

five classical steps of lean manufacturing are expanded by a dedicated engineering to scale step, that

highlights the importance of incorporating scalability into early product development. Key value for

the customer is generated by a modular, high performance propulsion technology that combines

high capability (large total impulse and high impulse density), high adaptiveness (throttling in specific

impulse and thrust), modularity (used as standalone thruster or in clusters enabled by bus design), as

well as attractive price point, both in direct cost (fixed low price offer) and reduced integration cost

enabled by solid, inert propellant and fast delivery cycles of two months or lower.

This value generation is succeeded by value stream analysis, analyzing required production steps

and flow for design throughputs with according buffers, including the identification of bottlenecks

and impact. Such analysis needs to be concluded to a level of detail where for example the screw-

locking of a glue is divided into the amount of minutes it takes an employee to mix the glue for one

batch of thrusters, then the amount of minutes he takes per thruster to apply the glue, the amount of

minutes he or she takes to load the thrusters into a curing oven and then the process time of the oven

used for curing the glue.

M O D U L A R D E S I G N

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14 15

Based on this, the production line is optimized for uninterrupted flow, adjusting bottleneck process

steps and culminating in the finalized production layout. The resulting ENPULSION production line

is a pull-based manufacturing line, in which subassemblies are produced independent of customer

projects up to late assembly stages, enabling shortened customer cycles.

By placing orders, customers pull requested thrusters in suitable configuration from the pool of pre-

assembled and stored thruster parts, triggering the final assembly and acceptance test flow. This

manufacturing line design allows total thruster cycle times including final assembly and standardized

acceptance testing within two weeks, generating unmatched short delivery cycles.

Within the entire manufacturing process, the agile implementation of heritage quality processes based

on inspection point principles that are seamlessly into incorporated in the production flow as well as

tools to continuous improvement result in high quality of delivered products as well as continuous

improvement of the production line satisfying the teams strive for perfection.

These classic steps of lean manufacturing are based on a complying engineering approach, which

introduces the mindset of large-scale production into the early stages of product development and

design stages.

L A R G E - S C A L E P R O D U C T I O N A P P R O A C H

ENPULSION thruster products are designed in a modularity manner both on thruster and subsystem

levels, and scaling between thruster products is accomplished by a philosophy of multiplication of

core components and processes. This not only allows to maintain heritage of key components on a

technological basis but is also in-line with the batch-based production line design.

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16 17

IMPLEMENTATION IN THE ENPULSIONMANUFACTURING PROCESS����������������������������������������

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Implementation of lean manufacturing principles

Engineering processes at ENPULSION are designed in accordance to this lean

manufacturing philosophy, linking the key areas with corresponding focal

points. In the interaction between processes and technology, the focus is laid

on continuous improvement.

The interaction between people and processes is focused on short develop-

ment cycles, whereas the interface between people and technology is domi-

nated by a focus on quality.

C O N T I N U O U S I M P R O V E M E N T

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18 19

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Manufacturing flow at the ENPULSION production line

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20 21

Based on these principles, the manufacturing process and scalability for IFM thrusters at ENPUL-

SION can be discussed. In step 1, automatized incoming inspection optimized for design throughput,

short non-conformance reporting with direct link to suppliers enables compliance with high heritage

quality processes, 100% part inspection and engineering feedback, while allowing the required high

throughput.

In step 2, emitters, which are the core component of the IFM technology, are manufactured from

incoming parts. These complex manufacturing steps are performed in parallel batches, including

aligned inspection plans, to achieve nominal throughput.

The same scaling principle applies to step 3, in which the propellant is loaded into the emitter in a

complex vacuum process. The semi-finished emitters are then scheduled to undergo a first charac-

terization testing in vacuum facilities in step 4, in which average process times, such as evacuation of

production chambers, are decreased by testing in batches and automatized test scripts.

Steps 2 to 4 strongly benefit from the design to scalability approach of the IFM technology, which

results in significant share of subassemblies across different thruster products.

In a further step, emitters are characterized using topology scanning methods and gathered data is

used to establish performance predictive models assisting emitter selection for early identification of

unsuited emitters.

Selected emitters are stored together with all other preassemblies ready for final thruster assem-

bly which is initiated by customer pull in the requested configuration. The streamlined design of the

thruster allows short assembly times within hours, enabled by the Kanban based manufacturing flow.

After final assembly, thrusters are undergoing acceptance testing in step 7, which can incorporate

customer provided mission realistic test levels, and is performed in batches. In a next step 8, the

thrusters are undergoing vibration testing, which is again conducted in parallel to increase through-

put, followed by final functional firing testing in vacuum facilities in final step 9.

Throughout steps 7-9, thrusters are assigned to customers, and fully digitalized non-conformance

reporting using agile processes and rapid decision cycles are in place, with a replace philosophy in

case of major non-conformances.

Step 10 is a streamlined final inspection, packaging and shipping step, in which a standardized pro-

cess together with close cooperation with logistics partner allow a maximum on flexibility as well as

minimum process times. Shipping specifications and packaging has been developed with significant

input from customers to align with respective receiving and incoming inspection processes.

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ENPULSION has successfully introduced a high rate production of a high-performance electric pro-

pulsion technology. Based on value stream analysis, a scalable production line design has been im-

plemented that scales to mega constellation production rates. Lean manufacturing philosophy allows

to implement a product lifecycle philosophy that combines New Space agility with heritage quality

processes, while providing high customer value in terms of product performance, cost reduction and

short cycle times.

It can be assumed that this example is largely representative for the industrialization of any other pro-

pulsion technology that is planned to be made available for large constellations. The presented case

study is however benefitting from the fact that the used FEEP propulsion system is lacking any fluid,

pressurized or toxic propellants and the evaluation of additional means to handle such propellants

and tanks in integrated gas-based propulsion systems are therefore not included in this discussion.

CONCLUSION

w w w . e n p u l s i o n . c o m


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